Core manufacture



Oct. 17, 1967 M.

E. wAslLlslN ETAL Re. 26,287

CORE MANUFACTURE Oct. 17, 1967 M. E. wAslLlslN ETAL Re. 26,237

CORE MANUFACTURE Original Filed Sept. 21, 1955 8 Sheets-Sheet 2 MICHAELE.WASILIS|N DONALD E W RNZ BY o V ATTO NEY INVENTORS Oct- 17, 1957 M. E.wAslLlsm ETAL Re. 26,287

CORE MANUFACTURE 8 Sheets-Sheet 5 Original Filed Sept. 21, 1955INVENTORS MICHEL E.WSILIS|N DONLD E.WERNZ ATTO EY C- 17, 1967 M. E.wAsILIsIN ETAL Re. 26,287

CORE MANUFACTURE Original Filed Sept. 21, 1955 8 Sheets-Sheet 4INVEN'T'ORS MICHAEL E.WASILI$IN DONLD E WERNZ AT'ro NEY OCL 17, 1967 M.E. wAslLxslN ETAL. Re. 26,28?

CORE MANUFACTURE Original Filed Sept. 21, 1955 8 Sheets-Sheet 5INVENTORS MICHAEL E. WASILISIN DONLD E.WERNZ A'I'TO NEY Oct. 17, 1967 M.E. wAsILIsIN ETAL Re. 26,287

CORE MANUFACTURE 8 Sheets-Sheet 6 Original Filed Sept. 21

INVENTORS MICHEL E.WASILISIN DONLD E. WERNZ ATTO NEY Oct. 17, 1967 M. E.wAsILIslN ETA.

CORE MANUFACTURE Original Filed Sept. 21, 1955 IIO V. SP

440 V. 3pH.

8 Sheets-Sheet 7 DISCONNECY SWITCH STRTER CR-S FROM FCTORY AIR SUPPLYIIO V. TO LIMIT SWITCHES To vMo'row 44 440 v.

Poor s ITcHEs Fs-I g Fs-a AIR HOS-E TO CYLINDER 90 INVENTORS MICHELE.WSILI$IN DONLD E. WERNZ CORE MANUFACTURE 8 Shaets-Sheet 8 OriginalFiled Sept. 21, 1955 mn II RV! MICHAEL E. WSILISIN DONLD E. WERNZ UnitedStates Patent O 26,287 CORE MANUFACTURE Michael E. Wasilisin and DonaldE. Wemz, Baltimore County, Md., assiguors to Martin-MariettaCorporatiou, a corporation of Maryland Original No. 2,780,716, datedFeb. 5, 1957, Ser. No. 535,638, Sept. 21, 1955. Application for reissueOct. 15, 1958, Ser. No. 767,495

9 Claims. (Cl. 219-83) Matter enclosed in heavy brackets II] appears inthe original patent but forms no part of this ressue specification;matter printed iu itallcs ind'icates the additions made by reissue.

This invention relates to an improved method of seamwelding corrugatedmetallic foil sections together to form honeycomb core havingsymmetrical cells, and to the machine for carrying out this method.

In the past, metallic honeycomb core has been extensively used in theconstruction of airplanes and similar applications where weight is animportant factor. The core material in most instances has beenconstructed of corrugated aluminum foil sections assembled into ahoneycomb-like Structure, with abutting valleys and crests of adjacentsheets bonded together by a thermosetting adhesive to form a series ofcells between the sections. The adhesive, when hardened or set, willbond the corrugated sections into a cellular core having considerableStrength.

This type of core has been used frequently in aircraft Wings, tailsurfaces, and flooring. For application in wings, for instance, the coreis first shaped such as by the used of a band saw, into a substantiallyairfoil-shaped cross-section, having vertically extending cells. Theshaped core is then covered with the uppe-r and lower skins of the wing,with the cells of the core residing in a vertical arrangement andextending between the skins. A thermosetting adhesive such as FM-47 isused to bond the skins to the core material. The constituents of theWing Structure are assembled in the proper relationship in What is knownas a bonding fixture and in this fixture, the wing Components aresubjected to heat and pressure to cause the adhesive to set and therebybring about the formation of a untary Structure.

For Operations in which no substantial temperature is involved, theabove-described bonded alumnum core has proven quite satisfactory. Whenhigh temperature and stress conditions are to be encountered, however,it becomes necessary to employ core Whose foil sections are made ofalloy steel, titanium and its alloys, or corrosionresistant type alloys.Such foil sections Would preferably be seam-welded together.

Although it is becoming increasingly desirable in the aircraft industryto employ honeycomb core made of high Strength material, the productionof such core has lagged considerably. This is principally due to thefact that it has been very difl'icult to maintain the alignment of thecorrugations of two adjacent sections of foil so that the abuttingapices of the sections, i.e., the valleys and crests, can be weldedtogether to form symmetrical honeycomb cells. Also, it has beendiflicult to dissipate satisfactorily the heat added to the core duringa resistance welding Operation so that burning of the core Will beentirely prevented.

In an attempt to circumve-nt the dilficulties encountered in the weldingof preformed corrugated steel sheets, alternative procedures have beenproposed. For example, one procedure has been to construct the core fromflat metal sheets that have been spot-welded along spaced parallel linesand then separated to form the expandedcell type of cellular core. Sucha procedure is not only painstaking and slow, but also results innonuniform cells of irregular placement. Further, in order that thesheets ICC can be satisfactorily separated so as to form theexpandedcell type of core, it is necessary to use sheets of annealedmaterial.

In contrast with the expanded-oell type of core, according to thepresent invention core can be made from corrugated metal foil at areasonably rapid rate. The resulting cells are quite symmetrical in sizeand placement, and if desired, can be made of almost perfect hexagonalconfiguration. Also, by using the present invention, core can be made ofhardenable materials, of the type which could be hardened either by heattreatment or by cold working. Because of the regularity of the cells andthe greater Strength of the materials involved, the instant core hassubstantially greater Strength qualities than are present in theexpanded-cell type of core.

A plurality of elongated fingers of conductive material are used tosupport the corrugated metal foil sections during the seam-weldingOperations, and these fingers form one of the electric terminals of theWelding machine. The iingers not only maintain the apices of adjacentsections of corrugated foil in alignment, but also conduct away heatfrom the core to keep it from overheating.

An object of this invention is to provide a method by which honeycombcore having cells symmetrical in size and placement can be Constructedrapidly from preformed corrugated members.

A more specific object of this invention is to provide a method by whichvalleys and crests of adjacent corrugated metal members can be placed inabutting algned relationship and then seam-welded together so as to forma core having cells symmetrical in size and placement.

Another object of this invention is to provide a seam- Welding machineby means of which the valleys and crests of adjacent corrugated metalmembers may be maintained in alignment and then seam-welded so as toform a core having cells symmetrical in size and placement.

Another object of this invention is to provide a method and a machinefor carrying out the method by which honeycomb core having cellssymmetrical in size and placement can be rapidly Constructed frompreformed corrugated members of hardenable metal.

The method according to this invention can comprise the steps of placinga section of corrugated metal foil on a set of spaced, substantiallyhorizontally disposed fingers of electrically conductive material, sothat the lower portions of the corrugations extend down between thefingers while the upper portions of the corrugations rest upon thefingers. A second set of electrically conductive tingers are placed soas to rest in the lower portions of the corrugations of said section,and a second section of corrugated metal foil is placed on the saidsecond set of fingers so that the lower portions of said second sectionare in alignment with and contacting the upper portions of saidfirst-mentioned section. An electrical terminai is placed in at leastone lower portion of said second section of foil at a location directlyabove at least one of the fingers of the first-mentioned set, and ismoved along said lower portion substantially in alignment with thelongitudnal axes of the respective finger of said firstmentioned set.Simultaneously, an electric current is passed between said terminai andsaid finger through both sections of foil whereby to seam-weld abuttingportions of said first and second sections together.

In order to secure the corrugated metal sections together at eachabutting location so as to form a series of cells between thesesections, the terminal is successively moved along each of the remaininglower portions of said second section, substantially in alignment withthe longitudinal axis of a respective finger, while electric current ispassed through both sections of foil to bring about the seam-weldingOperation.

Other sections of corrugated metal foil can be added to the now-weldedstructure according to this invention. In order that this may be done,the fingers of said firstmentioned set are removed from below said firstmentioned section of foil and then placed in the lower portions of saidsecond section, and then a third section of corrugated foil is placed onthe fingers of said firstmentioned set so that the lower portions of thecorrugations of said third section of foil are aligned with andcontacting the upper portions of the corrugations of said second sectionof foil. The electric terminal is then successively moved along each ofthe lower portions of said third section of foil while electric currentis passed between said terminai and said second set of fingers to weldthe abutting portions of corrugations of said second and third sectionstogether throughout the length of the sections. The core can be built upto the desired thickness by welding on additional sections of corrugatedfoil to create additional series of cells.

A seam-welding machine according to this invention can comprise amovable foil-supporting carriage and a welding carriage movable abovesaid supporting carriage in a direction transverse to the direction inwhich said supporting carriage moves, and in a plane substantiallyparallel to the plane in which said supporting carriage operates. Thesupporting carriage has a plurality of aligned, spaced notches orserrations in a transverse arrangement across the upper portion thereof,and each of the serrations is adapted to receive an elongated finger ofelectrically conductive material. A plurality of these fingers, whenplaced in a closely spaced parallel arrangement in said serrations,forms a support for a first section of corrugated foil.

The welding carriage is movable in a direction substantially parallel tothe longitudinal axes of the said fingers, and has a plurality ofwelding electrodes. Each of said electrodes, when fingers of thesupporting carriage have been moved into vertical alignment therewith,is adapted to move along a corrugation of a second corrugated foilsection Whose lower corrugations are aligned with and resting upon theupper corrugations of the first foil section.

Each of the electrodes and its respective finger is connected torespective output terminais of a source of electric current having apair of output terminais. By this arrangement, electric current can becaused to flow between each electrode and its respective finger, throughboth sections of foil resting on said supporting carriage, to seam-weldtogether the abutting corrugations resting below each electrode to forma series of cells between said foil sections.

Alternatively, the seam-welding machine can employ two sets of fingers,the fingers of each set being affixed in spaced relation in a supportbar. By this arrangement, the use of a support carriage having aserrated upper portion can be obviated, for each finger of each setderives its support from its support bar.

Other objects, features and advantages of this invention will beapparent from the following detailed description and the accompanyingdrawings of illustrative embodiments of the invention.

In the drawings:

FIG. l is a perspective view of one embodiment of a seam-weldingmachine;

FIG. 2 is a sectional view of the machine of FIG. l taken along sectionline 2--2;

FIG. 3 is a sectional view similar to that of FIG. 2 but with anotherfoil piece added to the core;

FIG. 4 is a sectional view similar to that of FIGS. 2 and 3. but withstill another foil piece added to the core;

FIG. 5 is a perspective view of a preferred embodiment of a seam-weldingmachine;

FIG. 6 is a side elevation view partly in section of the machine of FIG.5, this view being taken along section line 6-6;

FIG. 7 is a plan view of the machine of FIG. 5 with the motor and motormounting removed, this view being taken along section line 7-7 in FIG.6;

FIG. 8 is an end view of the machine shown in FIG. 6, this view beingpartly in section and drawn to a somewhat larger scale;

FIG. 9 is a view illustrating the arrangement of relays, switches andother Components on the control panel;

FIG. 10 is a schematic diagram of the control circuit of the weldingcarriage; and

FIG. 10a is a schematic diagram of the reversing switch of the weldingcarriage motor.

In FIG. 1 is illustrated an exemplary seam-welding machine 10 having acarriage 11 and two sets of metal fingers 12 and 13. Each set of fingers12 and 13 is rigidly secured in a respective mounting bar 12a or 13a sothat each set of fingers may be moved as a unit. Carriage 11 is made ofnon-conducting material and is movable generally in the direction of thelongitudinal axes of these fingers and over the entire length of thefingers. Copper arms 20a are Secured on the lower side of each end ofthe carriage, and these serve as mounting means for the two weldingwheels or discs 15, which are preferably of copper. Each disc 15 ismounted on an individual axle member 20, and each axle member isrotatable in its respective arm 20a. The inner ends of the axle membersare not in contact, and these ends are aflixed in non-metallic guidewheel 14. A separate source of welding current is connected to each arm20a, so that each welding disc can perform a seam-welding Operationindependently of the other disc. Although two discs have been used onthe instant machine, it is to be understood that one, three or even alarger numher of discs may be used satisfactorily.

The bars 12a and 13a may be supported by any desired means so that thefingers will be substantially horizontally disposed, and for clarity, nosupporting means for these bars have been shown in FIG. 1. Each set offingers can be mounted below one edge of the respective mounting bar, oralternatively, recesses can be provided in the upper and lower edges ofthese bars, between the fingers mounted therein, so that there will beno inteference with the placing of the fingers in the closely arrayed,interfitting relationship shown in FIGS. 1 through 4.

According to this invention, resistance welding techniques can beemployed to seam-weld a plurality of corrugated metal foil sectionstogether to form a honeycomb core. That seam-welding may satisfactorilybe done upon corrugated foil, one set of fingers is employed as thelower electrode of the resistance welding machine, while the other setof fingers is acting as the aligning means for maintaining the apices,i.e., valleys and crests of adjacent foil sections, in alignedrelationship that they may be satisfactorily welded together when thewelding discs are moved along the corrugations. Since it is usuallypreferable to manufacture honeycombcore that has hexagonal oralmost-hexagonal cells, the fingers 12 and 13 are substantiallyhexagonal in crosssection. Because of this, it is necessary to use foilthat previously has been corrugated so as to have three-sided or halfhexagonal corrugations, so that the foil can fit closely over the set offingers that are used to support it. When the first foil section 16 hasbeen correctly placed upon fingers 12 in the manner shown in FIGS. l and2, it fits closely over all of the fingers of the set with the upperportions or crests 17 of the corrugations resting upon the uppersurfaces of the fingers and the lower portions or valleys 18 extendingdown between the fingers.

In order that foil section 16 can be held closely against fingers 12,the set of fingers 13 (also of hexagonal cross-section) are placed so asto rest in the valleys 18 of foil section 16 in the manner shown inFIGS. 1 and 2. A second section of corrugated foil 19 then is placedupon fingers 13 in such a manner that the crests 21 of this section fitclosely against the upper surface of fingers 13 and the valleys 22extend down between the fingers so as to abut the crests 17 of foilsection 16. Welding carriage 11 is now placed upon foil section 19 inthe manner shown in FIGS. l and 2 with the guide wheel 14 resting in oneof the valleys 22 and the welding discs resting in valleys on eitherside of the valley in which the guide wheel rests. By this arrangement,the fingers 12 form a firm support for both sections of foil so that theweight of the welding carriage can press the abutting portions of thetwo foil sections tightly together that they may be satisfactorilywelded.

In the arrangement of the first and second foil sections shown in FIG.2, the fingers 12 form the lower electrodes, and the welding discs 15form the upper electrodes. The discs 15 are spaced sufliciently farapart that they do not rest in valleys that are immediately adjacent,but rather in valleys that are separated by an intermediate Valley. Thediscs are spaced in this manner inasmuch as it is not desirable that aseam-welding operation be performed simultaneously in two adjacentvalleys. Otherwise, the core might become overheated or the weldingcurrents might be induced to deviate from the straight vertical pathbetween a welding disc and its respective finger. The guide wheel 14travels in the intermediate Valley, and this wheel as prevouslymentioned, is made of a non-conducting material such as a phenolic orplastic material.

As shown in FIG. 1, a source 23 of electrical energy is provided for thewelding Operation, and output terminal 24, 24a and 25, 25a carry theelectrical potential from which the welding energy is derived. Terminals25 and 25a are joined together inasmuch as both are to be connected atthe same time to a set of fingers. Terminals 24 and 24a are at adifferent potential with respect to the terminais 25, 25a, and each ofthe terminals 24 and 24a are connected separately to one of the carriagearms a. Flexible leads 26 and 26a are connected to terminals 24 and 24a,respectively, and the other end of each lead is connected to an arm 20a.Lead 27 connects the common terminals 25, a to movable arm 31 of aswitch 28. Flexible leads 29 and 30 join terminals of switch 28 to thelower and upper sets of fingers 12 and 13, respectively, so that by theplacement of the arm 31 of the switch, one or the other of the sets offingers can be electrically connected to the terminai 25, 25a.

In the arrangement illustrated in FIG. 1, there is a difference ofelectric potential between each of the welding discs 15 and the lowerset of fingers 12, inasmuch as arm 31 of switch 28 is so placed that thefingers 12 are connected to terminals 25, 25a. Because of thisdifference in potential, current is induced to tiow between each disc 15and the finger 12 that is directly below each disc, the currentnecessarly flowing through both sections of corrugated foil and causingthem to be welded together. During the welding Operation, the carriage11 is moved along the uppermost foil section 19 with the welding discs15 rolling along the valleys 22 of this section, substantially inalignment with the direction of the longitudinal axes of the fingers 12.The guide wheel 14 assists in maintaining the discs traveling in a truecourse along the valleys.

In FIG. l, after the valleys 22 that are directly beneath the discs 15have been welded to the respective crests of foil section 16, thecarriage 11 is then moved or indexed so that all of the remainingvalleys of foil section 19 can be welded to the crests of foil section16 by the passage of welding current between the discs 15 and thefingers 12. When all of the abutting valleys and crests of section 16and 19 have been seam-welded, a new section of corrugated foil can thenbe added. The carriage 11 is removed from the position directly abovefoil section 19 and fingers 12 are removed from below section 16.Fingers 12 are then placed in the valleys 22 of section 19 in the mannerillustrated in FIG. 3, the fingers 13 CTt 6 supporting the now-weldedcore structure. A new section of corrugated foil 32 is then placed so asto rest closely upon fingers 12 with the valleys 34 of this foil sectionextending down between fingers 12 so as to rest in abutting relationshipwith the crest 21 of foil section 19. The carriage 11 is now placed inwelding position so as to rest on foil section 32, the welding discs 15and the guide wheel 14 each resting in a Valley 34. The contact arm 31of switch 28 is now shifted so as to be in contact with the terminai oflead 30, thereby causing the fingers 13 to become the lower electrode.The third section of foil 32 is now to be seam-welded to the second foilsection 19 so as to form a series of hexagonal cells between these twosections of foil, this being accomplished according to theabove-described procedure. It should be noted that the downward forcesapplied by the discs 15 in order to bring the abutting valleys andcrests into good contact for welding is borne by fingers 13, andtherefore is not dissipated through the core structure. Accordingly,there is little limitation on the number of corrugated foil sectionsthat may be added according to this invention.

FIG. 4 illustrates the manner in which a fourth section of foil 35 canbe welded onto the existing core. In this figure, the fingers 13 havebeen removed from their previous position beneath foil section 19 andplaced in the valleys 34 of foil section 32. Foil section 35 is thenplaced on top of fingers 13 with the valleys 37 of this section abuttingcrests 33 of foil section 32. The welding carriage 11 is then placed ontop of section 35, and this section of foil seam-welded to foil section32 according to the above-described procedure.

Although the fingers of sets 12 and 13 have been described as beingpreferably of hexagonal cross-section, it is to be understood thatfingers of other configuration may be used so that core material havingcells of a shape other than hexagonal may be made. For example, theupper and lower surfaces of the fingers can be oval, almost square, orsomewhat of sine Wave configuration. In such event, the foil used willbe corrugated in such a manner that it can rest closely against thefingers. The fingers are preferably of copper so that they will rapidlyconduct the heat produced by the welding Operation away from the foilsections thereby elminating overheating of the core. These may be alarge number of fingers in each set of fingers so that core material maybe made of substantial length. In place of discs 15, various other typesof devices may be employed. For instance, sliding contacts may be used,or gears having a close array of small teeth that will produceoverlapping spot welds (i.e., a seam-weld) may be employed.

As prevously mentioned, core material constructed from aluminum foil hasbeen quite satisfactory in the past when used in the construction ofairplane components, such as in wings. However, as aircraft speedscontinue to increase beyond the speed of sound and penetrate more andmore into the thermal barrier, it becomes desirable to have the corematerial constructed of metais having better capabilities at highertemperature than does aluminum, which shows little promise forstructures that are to be used at raised temperatures. Although a numberof alloy steels and corrosion-resistant type alloy steels havesatisfactorily been made into honeycomb material according to thisinvention, a precipitation hardening stainless steel known as l7-7PH,which is manufactured by the Armco Company of Middletown, Ohio has beenthe most satisfactory.

In the annealed state, the Structure of l7-7PH stainless steel ispredominantly austenite with lesser amounts of ferrite. This steel isunique in that transformation from the austenite can be accomplishedafter reheating in the range of 1200-1700 F. During such reheating,precipitation from the austenite affects the Composition of the steel tothe extent that transformation on cooling now starts at approximately200 F. and is sufi'iciently complete upon cooling to 60 F. that itpossesses desired properties. Transformation is accompanied by anincrease in Strength and hardness. 17-7PH stainless steel can readily bewelded by resistance welding, and excellent mechanical properties can beobtained in weldments. When this steel is welded after thetransformation treatment, it is not susceptible to cracking becausesteel of this low carbon content does not transform to martensite as aresult of welding.

The l7-7PH foil is received in the annealed condition and is transformedby heating it to approximately 1400 F. for approximately one andone-half hours and then cooling it to below 60 F. According to thepreferred procedure, the foil is then aged `at approximately 1050 F. forapproximately one and one-half hours, and then after cooling,successively apertured, corrugated, cut into sections of desired length,and then welded into a cellular core according to the above-describedmethod. Alternatively, the foil can be aged before it is corrugated orafter it has been welded into honeycomb core.

The foil is apertured by piercing or perforating substantially inaccordance with the patent to Theodore P. Pajak, No. 2,609,068, issuedon September 2, 1952, which is assigned to the assignee of the instantinvention. In honeycomb core, these apertures provide passages leadingfrom cell to cell and ontwardly of the core Structure, and are necessaryin order to liberate the vapors formed in the cells when the honeycombcore is bonded or brazed between two sheets to form a sandwichStructure. After the foil has been apertured, it is corrugated bypassing it through a corrugating machine in the nature of the machinedescribed and claimed in the Engel et al. patent, No. 2,609,3l4, issuedon September 2, 1952, and assigned to the instant assignee. Preferablythe foil is pierced by a rotary piercing machine that is operating injuxtaposition with the corrugating machine. Flat foil is fed into thepiercing machine and goes directly therefrom into the corrugatingmachine, and emerges from latter machine in a form that is ready to bewelded into honeycomb. Alternatively, the foil can be corrugated by useof a die tted in a pressbrake or punch press, but this is a much slowerprocedure.

In addition to 17-7PH stainless steel, other alloy steels such as AM350,AISI302, or AISI321 can be successfully used. In addition to steels,other high Strength materials such as titanium can be utilized to makehoneycomb core according to this invention. In the event that titaniumis to be used, the seam-welding of corrugated titanium foil sectionsmight preferably be done in an inert atmosphere, such as an atmosphereof argon or helium. The foil used has ranged in thickness between .0007"and .O06", with .0O3" foil usually being the most suitable thickness forstainless steel foils.

FIG. illustrates a preferred embodiment of a seamwelding machineaccording to this invention. This machine is generally identied bynumeral 41, and principally consists of a movable carriage 42 ofsubstantial length, a motor support 43 that supports driving motor 44,and a support frame 45 for a welding carriage. Motor support 43 has twolegs 43a which are bolted directly to support frame 45. Carriage 42 isarranged to carry the sections of corrugated foil that are to be madeinto honeycomb core, and this carriage travels back and forth below thewelding carriage support frame 45 upon horzontal rail members 46.

The rail members 46 are mounted upon support members 50 so that the railsurfaces will be spaced above the floor, this being done to permithoneycomb core of substantial dimension to be built up on this machine.A number of small wheels 49 are rotatably mounted at spaced locationsalong the bottom of carriage 42, and are so placed that the wheels Willroll along the rail surfaces as the carriage is moved back and forthwith respect to the support frame 45.

Carriage 42 principally consists of two spaced bars 47 joined togetherat each end by a spacer bar 48. Atop each of the bars 47 is a copper bar51 that is similar in size and length to the bar 47 to which it issecured. The copper bars 51 will hereinafter be referred to `as busbars. Along the top of the bus bars are a number of aligned, spacednotches or serrations 52 that are adapted to receive the numerousfingers 53 that are to support the sections of corrugated foil. Fiberstrips 83 are intermediate each bar 47 and its respective bus bar, andscrews 84 that secure the bus bars to the bars 47 have fiber sleeves 85and fiber washers 86. Nonconducting material is used in this manner sothat the bus bars 51 will be electrically isolated from the rest of themachine.

The finger 53 are to be laid in a parallel arrangement across the busbars, with one end of each finger resting on one of the bus bars 51. Theserrations in one bus bar are aligned with the serrations of the otherbus bar, so that when the fingers are placed with each end of eachfinger resting in a serration, there will be an orderly, parallel arrayof fingers along the top of carriage 42. A section of foil is then laidupon the fingers, the foil having been corrugated so that each of itscorrugations will fit closely upon a finger. This is best seen in FIG.8, wherein a short length of corrugated foil section 87 is shown restingupon fingers 53. A second set of fingers 53a is then laid on foilsection 87 and a second section of corrugated foil 88 laid upon thesecond set of fingers, with the valleys of section 88 aligned with andabutting the crests of section 87. By movement of welding carriage 57,the welding discs or electrodes 64 can be caused to simultaneously rollacross the upermost section of corrugated foil, thereby to bring aboutthe welding of the apices of the uppermost section of foil to the apicesof the section directly beneath it, the welding current passing betweeneach disc and the finger directly under the disc, through both foilsections.

After all of the abutting apices of sections 87 and 88 have beenseam-welded together to form and initial layer of cellular honeycombcore, one or more additional sections of corrugated foil can then beadded to this core. To do this, the fingers 53 are removed from theposition below foil section 87, allowing the newly-formed core to dropdown somewhat until the fingers 53a come to rest in the serrations 52.The fingers 53 then are placed in valleys of section 88 to act asalignment means and then an additional section of corrugated foil (notshown) is placed upon section 88 in such a manner that the valleys ofthe new section are aligned with and abut the crests of `section 88. Thevalleys of the new section then are searn-welded to the crests ofsection 88 by Operation of the welding carriage 57. Additional sectionsof foil can be added in the same general manner, with the honeycomb corebeing built up between the bus bars 51. This is best seen in FIG. 6,where a core consisting of a number of sections that have been weldedtogether is shown.

The welding carriage 57 rests in a welding carriage support frame 45,and is movable therein back and forth across the corrugated foil restingon carriage 42. The support frame rests on four upright posts, the twoposts 54a being located on the front side of the machine and the twoposts 54b being located on the rear side. The posts are secured by anglemembers 55 to the rail members 46. The support frame 45 is movablevertically upon the upper ends of the posts, such movement being broughtabout on occasion by means of a linkage 56. Linkage 56 will be describedin greater detail hereinafter, and sufilce it to say that the supportframe and welding carriage are periodically raised to permit the weldingdiscs 64 of the welding carriage to clear the foil sections supported oncarriage 42., that latter carriage can be indexed along rail members 46.

The support frame 45 has two side members 58, which are joined at theirfront end to member and at their rear end to the member 71, by means ofscrews or bolts 108. Generally U-shaped brackets are Secured to theexterior sides of side members 58, and in these brackets, the ends ofposts 54a and 54b are vertically slidable as the support frame is raisedor lowered. Since the Weight of the support frame is a consideration,the members 58, 70 and 71 are preferably made of a light metai such asaluminum, rather than of steel.

Referring to FIG. 7, the welding carriage 57 rests intermediate the sidemembers 58 of support frame 45. Formed in each side member 58 is alougitudinal slot 5821 along which the welding carriage travels` Bearingmembers 59 form the sides of the welding carriage that are adjacent themembers 58 of the` frame and these are joined at front and rear by endmembers 72 and 73, respectively. These end members preferably are madeof fiber or plastic. In cross-section, the members 59 of the carriagehave somewhat of a T-shaped Configuration. The leg 59a of each T ishorizontally disposed, and is closely fitted in its respectivelongitudinal slot 58a. See FIG. 8. The arrangement is such that thewelding carriage can slide virtually the length of frame 45, without anydegree of sideways or lost motion with respect to the frame.

Located in the welding carriage are electrode support bars 61 and 62,which are of a nonconducting material such as polystyrene. Each supportbar is non-rotatably supported at its ends by the members 59, and eachbar supports a plurality of bus bars 63. Six bus bars 63 are preferablyused in the instant machine, three being carried by each of the supportbars and placed in overlapping relationship as illustrated in FIG. 7.Rotatably mounted on each of the busses is a welding disc or electrode64. These six discs have aligned axes, and when the welding carriage isoperated, these discs roll along the corrugations of the uppermostsection of foil resting on carriage 42. The bus bars 63 are preferablyspaced on their support bars a distance equivalent to the distancebetween two serrations 52. This is done because it is desirahle for thediscs 64 to rest in alternate valleys as shown in FIG. 8.

So that two foil sections can be welded together by a current passingbetween the discs 64 of the upper busses and the fingers 53 resting onthe lower busses 51, a resistance welding arrangement in the generalnature of the one illustrated in FIG. 1 is provided. The lower bus bars51 are electricaily interconnected so as to be at the same potentiallevel` These bus bars act as a common or ground connection for thefingers that are placed thereon, for when resting on the bus bars 51,the fingers are in intimate contact therewith. The upper bus bars 63preferably are not connected to a common terminal, but rather each isconnected to a separate power supply so that a desirable amount ofcurrent can be made to flow between each of the welding discs 64 and itsrespective finger. For instance, six transformers (not shown) can beprovided, with one terminal of the secondary of each transformerconnected to the lower bus bars 51, with the remaining terminal of thesecondary of each transformer connected to one of the upper bus bars 63by a cable 99. Because of this arrangement, there will be no occasionfor a substantially different amount of current to flow between any onewelding disc and its respective finger, and any other disc and itsfinger. However, a single transformer may be employed to supply thewelding current for all the discs if such be desired. Welding contactor107, shown in FIG. 10, is operatively connected to the switchresponsible for connecting the primaries of the welding transformersacross the line.

By the above described welding arrangement, seam welds (i.e.,overlapping spot welds) can be performed at a normal rate that is twotimes the line frequency. In other words, if 60 cycle current isemployed to energize the primaries of the welding transformers, spotWelds will be performed at the rate of 120 welds per second.

Where other seam-weld spacing, or other welding rates are desired,conventional seam-welding control principles may be employed. As is wellknown in the welding industry, welding rates in many welding machinesmay be altered by varying thyratron grid control multivibrator rates. Ifit is desired to have an arrangement in which the voltage of the weldingelectrodes may be changed, saturable core reactors, resistances, orstored energy level systems may be used.

Each of the upper busses 63 tions, an upper portion 93 that respectivesupport bar 61 or 62, which is rotatable with respect to portions 93 and94 of each bus 63 portion has a hole therein so that assembled onto asupport bar. A is located in each upper portion locked to the supportbar. This not only prevents the rotation of this portion, but alsoinsures that the upper busses will not be accidentally displaced alongthe support bar. The lower portion 94 of each bus is rotatable aroundthe support bar for a comparatvely small number of degrees, andadjustment screws threaded into end members 72 and 73 of the weldingcarriage make it possible to adjust the lowermost position each lowerportion 94 can assume. A small spring (not shown) is fitted between eachset of upper and lower members to bias the lower member downwardly, andby means of spring adjustment screw 96 located on each upper position93, the spring pressure biasing the respective lower member downwardlycan be regulated. A welding disc 64 is rotatably mounted upon each lowerportion, and because of the Spring bias, as each welding disc rollsalong a corrugation of the foil, it presses tightly against the foil tosuch an extent that the abutting apices of the two foil sections will beplaced in firm contact with each other and with the finger thereunder.

In the instant machine, the serrations 52 on the carriage 42 have beenplaced .4l4" apart, center-to-center. Carriage 42 is approximately 11'long, and the rails 46 approxirnately twice that length. Assuming thereis about 10' of usable space along the top of carriage 42, approximately290 fingers can be accommodated in serrations 52. divided by .414"=290.)

The fingers are preferably made of copper in 8" lengths, having a Mtcross section. The fingers used in the instant machine have been alteredinto a modified hexagonal or squarecell cross-section by fiattening eachof the four corners of a square cross section to the extent of .060".The scrrations 52 have been shaped to receive fingers of suchConfiguration, and the foil to be used therewith is corrugated to fitclosely over the fingers when the fingers are resting in the serration.In FIG. 6 is shown a finger 53 resting across the bus bars 51, and inFIG. 7 a small number of fingers are shown residing in a parallel arrayupon carriage 42. As should be evident, the number of fingers usedduring the manufacture of honeycomb core is dictated by the length ofcore that it is desired to manufacture.

To accomplish the welding together of two corrugated foil sections, thewelding carriage 57 is movable forwardly and rearwardly in the supportframe 45 so that the welding discs 64 can be moved across the corrugatedfoil section in both directions. The moving of the welding carriage isaccomplished by means of reversible motor 44, the shaft 65 of which isdirectly connected to a spur gear 66 located on the rear side of themachine. Meshing with gear 66 is a larger gear 67 Whose hub or bushing68 is internally threaded in order to receive threaded shaft 69. The hub68 is located in end member 71 of support frame in such a manner thatwhile it can rotate, it is restrained against longitudinal movement.Therefore, as the motor causes gears 66 and 67 to rotate, the hub 68 ofgear 67 is likewise caused to rotate thereby to cause shaft 69 to movelongitudinally. Depending on the direction of rotation of motor 44, thewelding carriage can be caused to move either in the forward or in thereturn direction. Shaft 69 is bolted directly to end member 72 of thewelding carriage, inasmuch as this shaft does not rotatc.

is eomposed of two poris tightly secured to its and a lower portion 94the upper portion. The are interfitted and each both portions may be setscrew (not shown) 93 so that it can be As previously mentioned, linkage56 is responsible for moving the welding carriagc up and down on posts54a and 54b. An air cylinder 90 is located intermediate the posts 54a onthe front side of the machine. See FIG. 6- Upon high pressure air beingadmitted to cylinder 90, piston 74 is caused to move upwardly so as tobear against and raise arm 75. Arm 75 is secured in the central portionof rod 76, this rod being rotatably mounted in posts 54a. Upon rod 76being rotated by arm 75, it causes cranks 77 to rotate in a clockwisedirection as viewed in FIG. 6, this causing bars or links 78 on eachside of the welding carriage to move so as to bring about a similarrotation of cranks 79 which are Secured to rotatably mounted rod 81. Acam 82 is located adjacent each of the cranks in such a position as tobear on the underside of the side members 59 of the welding carriagesupport frame, and cause this frame to raise whenever the arm 75 isactuated by air cylinder 90. In other words, upon air cylinder beingactuated, the entire support frame 45 is caused to move up the posts 54aand 54b, thereby permitting the carriage 42 to be rnoved to a newposition underneath the welding carriage without interference fromwelding discs 64. One side of each of the posts 54a and 54b is providedwith an undercut or shelf 60 (see FIG. 8) which prevents the weldingcarriage from dropping down too far on the posts. Adjustment screws 7811are located in the links 78 to permit the length of these members to beadjusted so that the ends of the support frame will be raised evenly.

Electrical circuitry is employed to control the reciprocation of thewelding carriage 57 in support frame 45, to control the raising of thesupport frame, and to control the actuation of the switch or switchesused to connect the bus bars 51 and 63 to the source of electricity.Normallyclosed limit switches LS-l and LS-Z are mounted on mountingplate 103 and one of the legs 43a of the motor support 43, respectively,as shown in FIG. 7. The switches LS-l and LS-Z have switch arms 101 and102, respectively. Carns 91 and 92 are mounted on the upper surfaces ofbearing members 59 of the welding carriage, so that as this carriagenears the forward end of the support frame, limit switch LS-l will beactuated by cam 91, and as the carriage nears the rear end, switch LS-Zwill be actuated by cam 92.

Each cam has a tapered surface so that the arms 101 and 102 can begradually raised or lowered as cam 91 or 92 moves toward or away fromits respective switch arm. The cams have elongated slots 104 therein,through which extend mounting screws 105. The lower ends of these screwsare threaded into members 59, and by loosening the screws, the cams canbe moved to the desired position on the carriage. The screws 105 arethen of course retightened to maintain the cams in the correct positionon the welding carriage with respect to the limit switches.

The cams 91 and 92 should be so positioned that the motor 44 and thewelding current will be shut off after the welding carriage hastraversed the corrugated foil in either direction. For instance, whenthe welding carriage 57 rnoves toward the left as viewed in FIG. 7(i.e., moves in the forward direction), the welding discs 64 move towardthe left from the position shown in FIG. 6, along the corrugations ofthe uppermost section of foil so as to seam-weld the apices of thissection to the apices of the foil section directly below it. Then, asthe carriage 57 nears the front side of the support frame 45, the cam 91moves under the arm 101 of limit switch LS-l, causing this arm to raise,and thereby open the contacts of switch LS-l. As later described in moredetail, the opening of these contacts not only brings about thedeenergizing of motor 44. but also deenergizes the welding contactor 107to shut off the welding current fiowing between each welding disc 64 andthe finger 53 then under each disc. Further, the opening of the contactsof LS-l bring about the deencrgizing of normally-open solenoid valve 89,

tiO

causing it to open and admit high pressure air to cylinder 90, whichopcrates to raise support frame 45 so that carriage 42 can be indcxed toa ncw position below the welding crzrriagc. Solcnoid valve 89 is anelectrically operated solcnoid air valve, of a type that is commerciallyavailable. lt is a three way valve, so that when energizcd, it not onlyshuts off the fiow of compressed air to cylinder 90, but also rele-usesto the atmosphere the high pressure air contained in cylinder 90, sothat the support frame can return to the lowered position.

The operator controls the movcments of welding carriage 57 by means offoot switches FS-l and FS-Z, which are not shown except in FIG. 10,where these switches appear schematically. It is the closing of FS-lthat causes the welding carriage to move from right to left in themanner described above. When the welding carringe has come to rest inthe raised position near the front side of the machine, and the carriagc42 indexed to a new position, the switch FS-Z is pressed to cause thecarriage to perform a welding Operation in the return or rcarwarddirection. The closing of FS-2 causes the support frame to drop fromthis raised position into its lowered position, and the motor 44 to beconnected so as to operate in the reversc direction. Such rotation ofthe motor causes the welding carriage 57 to move in the returndirection, resulting in the cam 91 moving away from arm 101 of switchLS-1. This latter occurrence allows contacts of LS-1 to reclose, andthereby energize contactor 107 to bring about a tlow of welding currentbetween the discs 64 and the iingers now below the discs, through bothsections of foil resting on the fingers. In each instance it is theclosing of the foot switch FS-l or FS-2 that causes the movement of thewelding carriage and the dropping of the support frame 45, the resultingforward or rearward motion of the welding carriage causing the limitswitch LS-l or LS-Z to close and cause the welding current to commence.

Referring to FIG. 10, the wiring diagram illustrating the circnit of thewelding carriage 57 is shown. This circuit is supplied from aconventional 110 volt single phase A.C. supply.

The detailed Operation of the welding carriage is as follows:

(l) The operator presses start button of switch 106, completing thecircuit to the coil of control relay CR-7, causing this relay to beenergized. The actuation of this relay causes holding contacts (TR-7 toclose across the start button to maintain a closed circuit, and alsocauses line contacts of relay CR 7 to close, thereby energizing theentire welding carriage circuit.

(2) The operator prcsses foot switch FS-l causing the coil of controlrelay CR-l to be energized. (The circuit of relay CR-l is completedthrough contacts LS-IA, which are normally closed.) CR-1 holdingcontacts then close across switch FS-l to maintain a closed circuit, andother contacts of this relay close to energize control relays CR-6F andCR-3.

(a) The closing of relay CR-GF causes normally-open contacts of thisrelay to close in the Circuit of motor 44, connecting this motor acrossthe 440 volt 3-phase A.C. line. The contacts CR-6F are shown in themotor Circuit, FIG. lOa. Motor 44 now opcratcs in the forward direction,thereby causing the welding carriagc 57 to commence movementtransvcrsely of carriage 42, npon which the corrugated foil sections arecarried.

(b) The closing of relay CR--3 causes contacts CR-3 to close, completingthe circuit to solenoid valve 89. Since the solenoid valve is normallyopen, upon being energized it causes the cessation of the flow of highpressure air to cylinder 90, thereby allowing welding carriage supportframe 45 to drop downwardly so that the welding discs 64 can come intocontact with the lower corrugations of the uppermost section of foilsupported by carriage 42.

Since motor 44 has been placed across the line and is 13 now turning, itcommences to move the carriage in the forward direction. When thecarriage has moved a comparatively short distance, cam 92 moves awayfrom the position below the arm 102 of normally closed limit switch LS2, allowing its contacts to close.

The closing of contacts LS-2B of switch LS 2 completes the circuit tocontrol relay CR 5, causing it to be energized. Contacts of relay CR 5close in the circuit of welding contactor 107, which causes weldingcurrent to flow between welding discs 64 and the respective finger thatis under each disc, thereby performing the scamwelding Operation.

Contacts LS-ZA also close, which are contacts located in the circuit ofcontrol relay CR-2.

The welding carriage 45 continues moving across carriage 42, andultimately cam 91 reaches the artn of limit switch LS 1, causing the armto raise and to open the normally-closed contacts of this relay.

Contacts LS-IA open to deenergize relay CR-I, Whose contacts open todeenergize relays CR-6F and CR 3.

The deenergizing of relay CR-GF causes the contacts CR-6F to open,stopping motor 44.

The deenergizing of relay CR-3 breaks the circuit to solenoid valve 89allowing it to open and admit high pressure air to cylinder 90, causingthe support frame 45 and the welding carriage to be moved into theraised position.

Contacts LS-IB open in the circuit of control relay CR-S, which causeswelding contactor 107 to be deenergized, this causing the cessation ofthe flow of welding current.

(3) The support frame 45 and the welding carriage 57 being in the raisedposition, the operator can now index the carriage 42 to a new positionso that a new seamwelding Operation can be performed. When carriage 42is in the correct position, the operator presses foot switch FS-2 whichcompletes the circuit to control relay CR-Z, causing latter relay tobecome energized. Holding contacts of this relay close across switchFS-2 to maintain a closed circuit, and other contacts of this relayclose in the circuits of the coils of control relays CR-6R and (IR-4.

(a) The closing of contacts CR-R in the motor circuit causes motor 44 tobe connected to the 440 volt line so as to turn in the opposite, orreturn direction.

(b) The closing of relay CR 4 causes the normallyopen solenoid valve 89to close, shutting ofl the supply of high pressure air to cylinder 90,bringing about the dropping of the welding carrage 57 into the weldingposition. The welding discs 47 are now returned to the position in whichthey contact the corrugated foil.

Since motor 44 is now rotating in the opposite or return direction, thewelding carriage 57 now starts to move in the return direction, and whenit has moved a comparatively short distance, cam 91 moves away from theposition below normally closed limit switch LS-l, allowing its contactsto close.

The closing of contacts LS-IB completes the circuit to control relayCR-S, causing it to be energized. Contacts CR-S again close in thecircuit of welding contactor 107, causing the welding current to flowbetween the return direction.

Contacts LS 1A also close, these contacts being located in the circuitof control relay CR-d.

14 it to open and admit high pressure air to cylinder 90, causing thesupport frame 45 and the welding carriage to be moved into the raisedposition.

Contacts LS-ZB open in the circuit of welding control relay CR 5, whosecontacts open to deenergize welding contactor 107, and thereby bringabout the ccssation of the flow of welding current.

(4) The welding carriage 45 again being in the raised position, theoperator can now index the carriage 42 to yet another position so that athird steam-welding operation can be brought about. This Operation willtake place with the welding carriage 57 again moving in the forwarddirection. When carriage 42 is in the desred position, the operatorpresses foot switch FS-I and the sequence of events as described inparagraph #2 (Supra) again take lace. p When it is desred to deenergizethe control circuit, it is only necessary to press the stop button ofswitch 106, which causes the Opening of the contacts of control relayCR-7.

Although a similar electrical arrangement can be used to index thesupport carriage 42 along rails 46, it has been found desirable,particuiarly when very thin foil is being seam-welded, to index thiscarriage by hand.

Honeycomb core is Constructed in this machine as follows:

The desred number of fingers 53 are laid in a close array in theserrations 52 of the bus bars 51. A first section of corrugated foil 87of desred length is then laid upon the fingers, with the foil restingclosely upon each of the fingers. A second set of fingers 53a is thenlaid in the lower portions of the corrugations of foil section 87 in thegeneral manner shown in FIG. 7. This second set of fingers isresponsible for keeping the first section of foil in close contact withthe fingers 53. A second section of corrugated foil 88 is then laid uponthe second set of fingers 53a so as to fit closely upon these fingers.The abuttng apices of these sections of foil are now ready to be weldedtogether.

The welding is accomplished first by moving the carriage 42 to a firstposition below the welding carringe. This is a position in which each ofthe six welding discs 64 is aligned with a valley of the second foilsection. The location of the carriage 42 in a position correctly alignedwith the welding discs 64 of the welding carriage may be readilyachieved by the use of alignment devices 97 and 98, which are located onone of the rail members 46 on either side of the welding carriagesupport frame 45. These devices principally consist of blocks 97a and98a which have spaced serrations on their undersides, and Operatinghandles by means of which the blocks can be clamped against the adjacentbus bar 51. Despite the fact that the supporting carriage 42 may belocated close to one end of the rail members 46, the serrations of theblock of at least one of the alignment devices can be brought intocontact with some of the serrations 52 of the adjacent bus bar 51 toachieve alignment.

Upon carriage 42 being correctly placed, the welding carriage 57 isready to be moved transversely across the carriage 42, with the weldingdiscs 64 rolling along the lower corrugations of the uppermost sectionof foil. This is accomplished by first energizing the control circuit ofthe welding carriage (FIG. 10), which is done by pressing the startbutton of switch 106 located on control panel 100. The operator thenpresses foot switch FS 1, which brings about the Operation of reversiblemotor 44 in the 15 flow of welding current between each of the weldingdiscs 64 and the fingcr that is then under each disc.

After the welding discs 64 have been moved by the welding carriagecompletely across the uppermost section of corrugated foil to seam-weldabutting apices of the two sections of foil supported by fingers 53, cam91 of the welding carriage reachcs arm 101 of limit switch LS--L causingthis normally closed switch to open and thereby to bring about thedeenergizing of motor 44 and the welding contactor 107. This also causesthe normally open solenoid 89 (FIG. 9) to be decnergized, therebyallowing it to open and adrnit high pressure air to cylinder 90. Latteroccurrence causes the piston 74 of the cylinder to raise, therebycausing the support frame 45 and the welding carriage to be moved intothe raised position.

The raising of the welding carriage and support frame allows thecarriage 42 to be indexed to a new position without interference fromthe welding discs 64. That the carriage may be correctly aligned withrespect to the welding carriage, the alignment dcvices 97 and/or 98 arefirst released and then reapplied when the carriage 42 is in the desirednew position, in order that precise alignment of the valleys of the foilsections with welding discs 64 can be achieved. It is worthy of note atthis point that the carriage 42 is to be indexed a distancecorresponding to twelve corrugations, inasmuch as six corrugations areseam-welded during each Operation of the welding carriage 57, and onlyalternate corrugations are welded due to the spacing of the weldingdiscs 64.

Upon the carriage 42 now being correctly aligned, the welding carriage57 is to be moved in the opposite or return direction that a second setof six abutting apices can be seam-welded together. This is accomplishedby pressing the foot switch FS-Z, which not only connects the motor 44so that it operates in the reverse direction, but also causes thesolenoid valve 89 to cut off the supply of high pressure air to cylinder90, thereby allowing the air in cylinder 90 to be vented to theatmosphere to permit the welding carriage 57 to descend into the weldingposition. After the carriage 57 has moved a comparatively short distancein the return direction, the cam 91 moves away from the position beneaththe arm of normally closed limit switch LS-l, allowing its contacts toclose and bring about the energizing of welding contactor 107. Thecarriage continues the return movement across the corrugated foilsections until cam 92 reaches LS-2, which is thereby opened to stop themotor 44 and the welding current, and to bring about the raising ofsupport frame 45. The carriage 42 then can be indexed to a thirdposition, and the welding carriage again operated, now in the forwarddirection. These Operations are continued until the alternate abuttingapices have been welded together through the entire length of thecorrugated foil sections. The carriage 42 is then selectively moved inthe return direction so that the abutting apices that were skipped whenthe carriage 42 was moved in the first direction can now be welded. Aspreviously described, additional sections of foil can be added to thecore formed by sections 87 and 88 by using each set of fingersalternately as the lower set and as the upper set of fingers. First, oneset is used as the lower electrodes as well as the supporting means,while the other set of fingers is being used as the means for aligningthe section of foil being added. Then, when a new section of core is tobe added, the lower fingers are removed from the position resting in theserrations, and are used for aligning the new section of foil.

It is to be understood that the foregoing detailed description and theaccompanying drawings are illustrative and that the combination andimprovements herein disclosed may be embodied in various other Wayswithout departing from the invention defined by the claims.

What is claimed is:

[1. The method of making seam-welded honeycomb core comprising the stepsof placing a section of corrugated metal foil on a set of spaced,substantially horizontally disposed fingers of electrically conductivematerial, so that the lower portions of the corrugations extend downbetween the fingers while the upper portions of the corrugations restupon the fingers, placing a second set of fingers in the lower portionsof said section, placing a second section of corrugated metal foil onsaid second set of fingers so that the lower portions of said secondsection are in alignment with and contacting the upper portions of thefirst-mentioned section, placing an electrode in at least one lowerportion of said second section of foil at a location directly above atleast one of the fingers of the first-mentioned set, moving saidelectrode along said lower portion substantially in alignment with thelongitudinal axis of the respective finger of said first-mentioned setwhile passing electric current between said electrode and said fingerthrough both sections of foil whereby to seam-weld abutting portions ofsaid first and second sections together] [2. The method of makingseam-welded honeycomb core comprising the steps of placing a section ofcorrugated metal foil on a set of spaced, substantially horizontallydisposed fingers of electrically conductive material, so that the lowerportions of the corrugations extend down between the fingers while theupper portions of the corrugations rest upon the fingers, placing asecond set of fingers of electrically conductive material in the lowerportions of said section, placing a second section of corrugated metalfoil on said second set of fingers so that the lower portions of saidsecond section are in alignment with and contacting the upper portionsof the firstmentioned section, placing an electrode in at least onelower portion of said second section of tfoil at a location directlyabove at least one of the fingers of the firstmentioned set, moving saidelectrode along said lower portion substantially in alignment with thelongitudinal axis of the respective finger of said first-mentioned setwhile passing electric current between said electrode and said fingerthrough both sections of foil whereby to scamweld abutting portions ofsaid first and second sections together, successively moving saidelectrode along each of the remaining lower portions of said secondsection, substantially in alignment with the longitudinal axis of arespective finger, to seam-weld said first and second sections togetherat each location where the upper portions of said first-mentionedsection and the lower portions of said second section abut, whereby tosecure said sections together so as to form a series of cells betweensaid first and second sections, removing said first-mentioned set offingers from below said first-mentioned section of foil and placing themon the lower portions of said second section, placing a third section ofcorrugated metal foil on the fingers of said first-mentioned set so thatthe lower portions of the corrugations of said third section of foil arealigned with and contacting the upper portions of the corrugations ofsaid second section of foil, successively moving said electrode alongeach of the lower portions of said third section of foil while passingan electric current between said terminal and said second set of fingersto weld said second and third sections of foil together so as to form aseries of cells therebetween, removing said second set of fingers frombelow said second section of foil and placing them on the lower portionsof said third section, placing a fourth section of corrugated metal foilon the fingers of said second form so that the lower portions of thecorrugations of said fourth section rest upon the upper portions of thecorrugations of said third section of foil, welding said third andfourth sections together so as to form a series of cells therebetween,and continuing to build up said core in thickness by welding onadditional sections of corrugated foil to create additional series ofcells] 3. A seam-welding machine for making honeycomb core material froma plurality of corrugated foil sections comprising a movable supporttngcarriage and a welding carriage movable above said supporting carriagein a direction transverse to the direction in which said supportingcarriage moves, and in a plane substantially parallel to the plane inwhich said supporting carriage operates, said supporting carriage havinga plurality of aligned, spaced serrations in a transverse arrangernentacross the upper portion thereof, each of said serrations being adaptedto receive an elongated finger of electrically conductive material, aplurality of said fingers, when placed in a closely spaced parallelarrangement in said serrations, forming a support for a first section ofcorrugated foil, said welding carriage being movable in a directionsubstantially parallel to the longitudinal axes of said fingers andhaving a plurality of welding electrodes, each of said electrodes, whenfingers of said supporting carriage have been moved into alignmenttherewith, being adapted to move along a corrugation of a secondcorrugated foil section Whose lower corrugations are aligned with andabutting the upper corrugations of said first foil section, meansconnecting each of said electrodes and its respective finger torespective output terminals of a source of electric current having apair of output terminals, whereby electric current is caused to flowbetween each electrode and its respective finger, through both sectionsof foil resting on said supporting carriage, to seam-weld together theabutting corrugations resting below each electrode to form a series ofsymmetrical cells between said foil sections.

4. A seam-welding machine for making honeycomb core material from aplurality of corrugated foil sections comprising a movable supportingcarriage and a welding carriage movable above said supporting carriagein a direction transverse to the direction in which said supportingcarriage moves, and in a plane substantially parallel to the plane inwhich said supporting carriage operates, said supporting carriage havingtwo spaced, longitudinally disposed bus bars on its upper portion, eachof said bus bars having a plurality of spaced serrations therein, withthe serrations of one bus bar aligned with the serrations of the otherbus bar, each set of two aligned serrations being adapted to receive anelongated finger of electrically conductive material, a plurality offingers, when placed in a closely spaced parallcl arrangement acrosssaid bus bars, forming a support for corrugated foil, said weldingcarriage being movable in a direction substantially parallel to thelongitudinal axes of said fingers and having a plurality of weldingelectrodes, each of said electrodes, when fingers of said supportingcarriage have been moved into alignment therewith, being adapted to moveacross said supporting carriage so as to seamweld together the abuttingapices of two sections of corrugated foil supported by said fingers,means connecting each of said electrodes and its respective finger torespective output terminals of a source of electric current having apair of output terminals, whereby electric current is caused to flowbetween each electrode and its respective finger, through both sectionsof foil resting on said fingers, to seam-weld the crests of the lowersection to the valleys of the upper section to form a series ofsymmetrical cells between said foil sections.

5. A seam-welding machine for making honeycomb core material from aplurality of corrugated foil sections comprising a movable supportingcarriage and a welding carriage movable above said supporting carriagein a direction transverse to the direction in which said supportingcarriage moves, and in a plane substantially parallel to the plane inwhich said supporting carriage operates, said supporting carriage havingtwo spaced, longitudinally disposed bus bars on its upper portion, eachof said bus bars having a plurality of spaced serrations therein, withthe serrations of one bus bar aligned with the serrations of the otherbus bar, each set of two aligned serrations being adapted to receive anelongated, removable finger of electrically conductive material, aplurality of fingers, when placed in a closely spaced parallelarrangement across said bus bars, forming a support for corrugated foil,said welding carriage being movable in a direction substantiallyparallel to the longitudinal axes of said fingers and having a pluralityof welding electrodes, each of said electrodes, when fingers of saidsupporting carriage have been moved into alignment therewith, beingadapted to move across said supporting carriage so as to seam-weldtogether the abutting apices of two sections of corrugated foilsupported by said fingers, means connecting each of said electrodes andits respective finger to respective output terminals of a source ofelectric current having a pair of output terminals, whereby electriccurrent is caused to flow between each electrode and its respectivefinger, through both sections of foil resting on said fingers, toseam-weld the crests of the lower section to the valleys of the uppersection to form a series of syrnmetrical cells between said foilsections, said core, as additional sections of corrugated foil arewelded thereto, being built up below said fingers, and being supportedthereby between said bus bars.

[6. A seam-welding machine for making honeycomb core material from aplurality of corrugated foil sections comprising a set of spaced fingersfor supporting corrugated foil, and a welding carriage movable in aplane adjacent the plane of said fingers and in a directionsubstantially parallel to the longitudinal axes of said fingers, saidcarriage having a plurality of welding electrodes adapted to move alongsaid fingers so as to seam-weld together the abutting apices of twosections of corrugated foil supported by said fingers, means connectingeach of said electrodes and its respective finger to respective outputterminals of a source of electric current having a pair of outputterminals, whereby electric current is caused to flow between eachelectrode and its respective finger, through both sections of foilresting on said fingers, to seam-weld together the abutting corrugationsresting below each electrode to form a series of symmetrical cellsbetween said foil sections] [7. A seam-welding machine for makinghoneycomb core material from a plurality of corrugated foil sectionscomprising a set of spaced fingers for supporting corrugated foil, and awelding carriage movable in a plane adjaceut the plane of said fingersand in a direction substantially parallel to the longitudinal axes ofsaid fingers, said carriage having a plurality of welding electrodesadapted to move along said fingers so as to seam-weld together theabutting apices of two sections of corrugated foil supported by saidfingers, means for securing the lower of the two sections against saidfingers so that the lower portions of the corrugations extend downbetween the fingers while the upper portions of the corrugations restupon the fingers, means connecting each of said electrodes and itsrespective finger to respective output terminals of a source of electriccurrent having a pair of output terminals, whereby electric current iscaused to flow between each electrode and its respective finger, throughboth sections of foil resting on said fingers to seam-weld together theabutting corrugations resting below each electrode to form a series ofsymmetrical cells between said foil sections] 8. In all metal honeycombcore fabrcating machine, a work station, a feed mechanism for supportingan opposifely corrugated pair of transversely corrugated metal ribbonsin juxfaposilon at said work station with the nodes thereof in abutmentand for intermittently advancing said ribbons longtudinally through saidwork station a distance equal to a whole number multiple of the spacingbetween said corrugations, and means at said work station cyclicallyoperalve in timed relation to the movement of said strps to bond saidabum'ng nodes` together.

9. The machine defined in claim 8 wherein said bondz'ng means comprisesa bonding tool, means mounting said bonding tool for recprocalionbetween an operative position in engagement with a pair of abuttingnodes of such ribbons and an inoperative position remote from the pathof movement of said ribbons, and means operative in tirned relation withsaid ribbon advancing meann` to reciprocate said bonding tool betweenits operative and inoperative positions.

10. The machine defined in claim 8, wherein said bonding tool is anelectricai resistance welding head.

11. The machine defined in claim4 10 wherein said weldng head comprisesa pair of electrodes at least one of which is a roller and means forenergizing said electrodes when in operative position and wherein saidbonding tool reciprocating means is operative to advance said rollerelectrode along the engaged node while energized.

12. In the honeycomb core fabricating machine defined in ciaim 8, saidfeed mechanism comprising a plurality of pins adapted to be receivedwithin the cells defined by said ribbons at each side of said workstation, and means` for moving said pins to intermittently advance saidribbon through said work station.

13. In combination, a work station, means for supporting an oppositelycorrugated pair of transversely corrugated metallic ribbon sections injuxtaposition at said work station with the nodes thereof in abutment,means for advancing said strips through said work station in thedirection transverse to the corrugation's a distance equal to a wholenumber multiple of the spacing between adjacent corrugations, means atsaid work station intermittently operative in timed relaton to themovement of said strips to weld said strip portions together including apair of electrodes mounted for cyclicai movement langi- 20 tudinaily ofthe corrugations of said strips between an inoperative position remotefrom the path of movement of said strip and an operative positionembracing said abutting strip portions, and means cyclically operatve toenergize said electrodes when in said operative position to bond saidabutting strip portions together.

References Cited The following references, cited by the Examiner, are ofrecord in the patcnted file of this patent or the original patent.

UNITED STATES PATENTS 853,241 5/1907 Helberger 219-80 1,074,383 9/1913Rietzel 219-80 1,826,207 10/1931 Fassler 219-80 l,850,454 3/1932 Gross219-80 1,869,804 8/1932 Eksergian 219-80 2,065,546 12/1936 Young et al219 81 2,163,590 6/1939 Ganahl et al. 219' 82 2.423,870 7/1947 Blessing219-117 2,975,263 3/1961 Green et al 219-83 FOREIGN PATENTS 825,32? 12/1937 France.

RICHARD M. WOOD, Primary Examiner.

JOSEPH V. TRUHE, MAX L. LEVY, Examiners.

B. A. STEIN, Assistant Examiner.

